Comparison of Mil Mi-26 “Halo” and Sikorsky CH-53E Super Stallion [S]ave
| Attribute |  Mil Mi-26 “Halo” × |  Sikorsky CH-53E Super Stallion × |
|---|---|---|
| General | ||
| Manufacturer | MIL Helicopters | Sikorsky Helicopter |
| Model | Mil Mi-26 “Halo” | Sikorsky CH-53E Super Stallion |
| Country | Russia | United States |
| Manufactured from (year) | 1986 | 1981 |
| Manufactured to (year) | - | 2003 |
| Type | Military Helicopters | Military Helicopters |
| Icao | - | H53S |
| Performance | ||
| Engine | 2 × Lotarev D-136 turboshafts - | 3x 3 × General Electric T64-GE-416/ GE-416A / GE-419 |
| Power, hp (hp) | 11,240 | 4,380 |
| Avionics | - | Rockwell Collins Avionics |
| Max cruise speed (km/h) | 256 | 278 |
| Travel range (km) | 1,952 | 1,000 |
| Fuel economy (km/l) | 0.186 | 0.245 |
| Service ceiling (m) | 4,602 | 5,639 |
| Rate of climb (m/sec) | 7.73 | 12.7 |
| Weights | ||
| Max take off weight (kg) | 56,000 | 33,340 |
| Max payload (kg) | 20,000 | 14,515 |
| Fuel tank capacity (l) | 12,000 | 10,637 |
| Baggage volume (m³) | 6.16 | - |
| Dimensions | ||
| Seats | 9 | 55 |
| Seats - business class | 65 | - |
| Cabin height (m) | 3.2 | 1.98 |
| Cabin width (m) | 3.1 | 2.29 |
| Cabin length (m) | 12.1 | 9.14 |
| Exterior length (m) | 40.03 | 30.2 |
| Tail height (m) | - | 8.46 |
| Fuselage diameter (m) | - | 2.5 |
| Wing span (m) | 32 | 24.08 |
| Wing tips | No Winglets | No Winglets |
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